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General: Flexible platform option for the LUNA TUAS.
MTOW: Max. 125 kg.
Abmessungen: Length: 3,2 m, Height 1,1 m, Wideth 0,9 m.
Antrieb: 30 KW Heavy-Fuel Turbo-shaft.
Rotor: 3-Bladesystem, Rotordiameter 350 cm.
Enrurance: ca. 3 hours.
Guidance:
Preprogrammed (3D waypoint list) using high resolution digital maps or high resolution aerial images; and/or remotely controlled. Mission program can be altered in flight. Differential GPS navigation and/or data link auto tracking (via range and azimuth data), option for automatic return flight to base.
Avionik:
Inertial Navigation System, autopilot and aircraft system management are fully digital. Sensor package includes attitude gyro, rate of turn sensors, magnetic compass, air data sensors and accelerometers.
Payloads: Cameras: Tiltable sensor platform with up to 7 color zoom and IR zoom video, -arrays, -turrets, -high-definition, -hyperspectral, forward looking pilot color video. Synthetic Aperture Radar (SAR), SIGINT-sensors, CBRN-sensors.
Optional payloads:
Data link relay payload for beyond line-of-sight reconnaissance and communication, Encryption, GCS hand off function.
Data link:
Microwave link (C-band), tracking antennas in air vehicle and ground station. Command uplink, control and video/telemetry in real-time, jamming resistant.
Data link Range: > 100 km.
Take off and landing: ATOL, vertical.
Ground Control Station:
Modular LUNA TUAS GCS design to fit in any vehicle or container. Advanced human-machine-interface (HMI).